HULIANWANG DIGUI-06, 62328
Orbit data source: Space-Track
HULIANWANG DIGUI-06, 62328 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Mon, 16 Dec 2024 UTC via a CHANG ZHENG 5B/YZ-2 launch vehicle from the Wenchang Satellite Launch Center (WSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62328 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 HULIANWANG DIGUI-06
1 62328U 24240F 25340.61516813 .00000112 00000-0 22616-3 0 9992
2 62328 86.4974 48.1050 0001788 90.7159 269.4180 13.24415078 47156TLE epoch observation values (Epoch: 2025-12-06T14:45:50.526Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #240 in the year 2024 (2024-12-16 UTC)
HULIANWANG DIGUI-06 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2025-12-07 05:21:48.781Z | 186.516° SSW | 2025-12-07 05:27:48.781Z | 235.464° WSW | 44.087° | 2025-12-07 05:34:48.781Z | 359.451° N |
| 5 mins | 2025-12-07 14:58:48.781Z | 48.947° ENE | 2025-12-07 15:00:48.781Z | 66.758° ENE | 13.693° | 2025-12-07 15:03:48.781Z | 93.431° ESE |
| 12 mins | 2025-12-07 16:45:48.781Z | 358.562° N | 2025-12-07 16:50:48.781Z | 15.042° NNE | 44.76° | 2025-12-07 16:57:48.781Z | 178.584° S |
| 5 mins | 2025-12-07 18:36:48.781Z | 307.402° NW | 2025-12-07 18:38:48.781Z | 289.348° WNW | 14.35° | 2025-12-07 18:41:48.781Z | 262.288° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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